|
CATEGORY
|
DESIGN
SPECIFICATION
|
REFERENCE
CASR / FAR
|
|
SMALL
AIRCRAFT
|
Ø
Maximum
Certificated Take Off Weight
(MTOW) ≤ 12,500
Lbs ( ≤ 5,700 Kg )
|
§1.74; §
135.1
|
|
SMALL
AIRPLANES ( Fixed Wings) :
|
||
|
NORMAL AIRPLANE
|
Ø
Maximum
Certificated Take-Off Weight ≤ 12,500
Lbs
( ≤ 5,700 Kg )
Ø
Seating Configuration ≤ 9 (excluding Pilot)
Ø
Technical Operation is intended for non-acrobatic maneuver
|
§ 23.3(a)
|
|
UTILITY AIRPLANE
|
Ø
Maximum
Certificated Take-Off Weight ≤ 12,500
Lbs
Ø
Seating Configuration ≤ 9 (excluding Pilot)
Ø
Technical Operation is intended for limited acrobatic menoeuver
|
§ 23.3(b)
|
|
ACROBATIC AIRPLANE
|
Ø
Maximum
Certificated Take-Off Weight ≤ 12,500
Lbs
Ø
Seating Configuration ≤ 9 (excluding Pilot)
Ø
Technical Operation is intended for acrobatic maneouver
|
§ 23.3(c)
|
|
SMALL
ROTOR CRAFTS (Helicopters) :
|
||
|
NORMAL ROTORCRAFTS
|
Ø
Maximum Weight ≤
6,000 Lbs
|
§ 27.1
|
|
|
||
|
LARGE
AIRCRAFT
|
Ø
Maximum
Certificated Take Off Weight >
12,500 Lbs
( > 5,700 Kg )
|
§ 1.45,
§ 121.1,
§ 135.1
|
|
LARGE
AIRPLANES (Fixed Wings):
|
||
|
COMMUTER AIRPLANE
|
Ø
Maximum
Certificated Take Off Weight ≤ 19,000
Lbs (≤ 8,600 Kg
)
Ø
Seating
Configuration ≤ 19
(excluding Pilot)
Ø
Technical
Operation is intended for non-acrobatic
maneuver
Ø
Propulsion
is multi-engine (n > 1), propeller-driven
|
§ 23.3(d)
|
|
COMMUTER AIRPLANE (operational)
|
Ø
Max Seating Capacity/Configuration ≤ 30 (excluding required crew member seat : Pilots & cabin attendants)
|
§ 135.3
|
|
TRANSPORT AIRPLANE
|
Ø
Maximum
Certificated Take-Off Weight > 19,000 Lbs, or
Ø
Seating
Configuration > 19 (excluding Pilot)
|
§ 25.1
|
|
CATEGORY
|
DESIGN SPECIFICATION
|
REFERENCE
CASR /
FAR
|
|
LARGE
ROTORCRAFTS (Helicopters) :
|
||
|
TRANSPORT ROTORCRAFT
|
Ø
Weight > 6,000 Lbs
Ø
Category A :
o
Weight > 20,000 Lbs, and
o
Passenger Seats
≥ 10
Ø
Category B
++ :
o
Weight > 20,000 Lbs, and
o
Passenger Seats ≤ 9
o
Comply with
Category A requirements of Subparts C, D, and F
Ø
Category B + :
o
Weight ≤ 20,000 Lbs, and
o
Pax Seats ≥ 10
o
Comply with
Category A requirements of §29.67(a)(2),
§ 29.87, § 29.1517, and Subparts C, D, E, and F
Ø
Category B :
o
Weight ≤ 20,000 Lbs, and
o
Passenger Seats
≤ 9
|
§29.1
|
|
|
||
|
PRIMARY AIRCRAFT *
-
Airplane,
-
Gliders,
-
Rotorcraft,
-
Manned-free Balloon,
|
Ø
Propulsion
o
The aircraft is
Unpowered ; or
o
The airplane
Powered by a Single, naturally aspirated engine, with stall speed Vso ≤ 61 knots as defined in § 23.49; or
o
Rotorcraft with
6 lbs/ft2 main rotor disc loading limitation, under SLDC (Sea
Level standard Day Conditions);
Ø
Weight ≤ 2,700 lbs (land-plane), ≤
3,375 lbs (sea-plane)
Ø
Seats ≤ 4 (including pilot)
Ø
Cabin is Un-pressurized
Ø
Operation is
intended exclusively for pleasure and
personal use. The carrying for persons or property for hire is prohibited.
|
§ 21.24 *
- Not yet adopted by CASR 21,Rev.-(ref. FAR Amdt up to 21-69)
* Primary Aircraft
introduced starting in FAR 21, Amdt
21-70.
|
|
RESTRICTED AIRCRAFT
|
Technical Operation is
intended for Special Purpose Operations, includes agricultural, forest and
wildlife conservation, aerial advertising; and any other operations specified
by the Director General.
|
§ 21.25
|
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